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The application of strain range partitioning method to torsional creep-fatigue interaction
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Zamrik, S. Y. |
| Copyright Year | 1975 |
| Description | The method of strain range partitioning was applied to a series of torsional fatigue tests conducted on tubular 304 stainless steel specimens at 1200 F. Creep strain was superimposed on cycling strain, and the resulting strain range was partitioned into four components; completely reversed plastic shear strain, plastic shear strain followed by creep strain, creep strain followed by plastic strain and completely reversed creep strain. Each strain component was related to the cyclic life of the material. The damaging effects of the individual strain components were expressed by a linear life fraction rule. The plastic shear strain component showed the least detrimental factor when compared to creep strain reversed by plastic strain. In the latter case, a reduction of torsional fatigue life in the order of magnitude of 1.5 was observed. |
| File Size | 3790364 |
| Page Count | 28 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19760023521 |
| Archival Resource Key | ark:/13960/t5w717s07 |
| Language | English |
| Publisher Date | 1975-10-01 |
| Access Restriction | Open |
| Subject Keyword | Structural Mechanics Range Extremes Torsional Stress Partitions Mathematics Fatigue Materials Thermal Cycling Tests Plastic Deformation Stainless Steels Creep Analysis Ntrs Nasa Technical Reports ServerĀ (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |